[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2019 , Vol. 39 >Issue 6: 142 - 145

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.06.031

Application of Piezoelectric Bimorph in Guided Bullets

  • CHENG Gang ,
  • CHEN Chao ,
  • CHEN Heng
Expand
  • State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received date: 2018-11-20

  Online published: 2025-05-12

Fold

Abstract

In order to realize the precise control of micro-caliber high-elastic ammunition,the application field of extended piezoelectric bimorph is proposed.Based on the variable centroid control mechanism,a tuning attitude device for small-caliber high-rotation stable missile is proposed.The solution generates a change in the mass moment by the piezoelectric bimorph oscillating mass,and the amplification of the output torque is achieved based on the centrifugal field action.The structural dynamics model of the dual-wafer-mass system was established and the finite element simulation analysis was carried out.A rigid body dynamics model of the warhead (the warhead part) was established.The theoretical analysis results show that the attitude system can meet the requirements of attitude adjustment and can amplify the output torque.

Key words： piezoelectric bimorph; moving mass; high-speed spinning bullets; adjustment control

Cite this article

CHENG Gang , CHEN Chao , CHEN Heng . Application of Piezoelectric Bimorph in Guided Bullets[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(6) : 142 -145 . DOI: 10.15892/j.cnki.djzdxb.2019.06.031

[an error occurred while processing this directive]

References

Publishing order | Descend order by publishing year | Descend order by cited within
[1]
邓以高, 田军挺, 王亚锋, 等. 飞行器姿态控制方法综述[J]. 战术导弹控制技术, 2006(2) :7-13.

[2]
魏泽宇, 冯秀莲, 刘山, 等. 制导子弹的发展现状与关键技术[J]. 飞航导弹, 2015(10):38-42.

[3]
BARRETT R, LEE G. Design and testing of piezoelectric fli ght control actuators for hard-launch munitions[C]// FLATAU A B.Proceedings of SPIE Vol.5390 (Smart Structures and Materials 2004:Smart Structures and Integrated Systems).[S.l.]:SPIE,2004:459-470.]

[4]
HU K M, WEN L H. Scheme design and mechanical analysis about new-type bullet based piezoelectric rudder actuator[J]. Journal of Mechanical Engineering, 2015, 51(21):104-112.

[5]
ZHAO H C, WANG T, FAN S L. Modeling and adaptive sliding mode control of varyin gcentroid spinning warhead[J]. Science & Technology Reviem, 2009(5):43-46.

[6]
ZHAO H C, SHI X J, FAN S L. The variable centroid control of a spinning warhead based on a new collocating mode[J]. Aerospace Control, 2011, 29(4):3-7.

[7]
Zhao Cs. Ultrasonic motors technologies and application[M]. Beijing: science press, 2007.

[8]
YI Y, ZHOU F Q, ZHOU J. Motion analysis on moving center of mass controlled missile[J]. Aerospace Control, 2000, 18(3):1-5.

Options
Outlines

/

〈 〉

[an error occurred while processing this directive]